AIAA-2005-1058 BOUNDARY LAYER DEVELOPMENT ON ROTOR BLADES OF A FOUR-STAGE LOW-SPEED AXIAL COMPRESSOR
17th, International symposium on air breathing engines ; 2005 ; Munich, Germany
2005-01-01
43 pages
Includes bibliographical references and index; Papers on CD-ROM
Aufsatz (Konferenz)
Englisch
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